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GB2045357B - Aircraft turbine engine mounting assembly - Google Patents

Aircraft turbine engine mounting assembly

Info

Publication number
GB2045357B
GB2045357B GB8006002A GB8006002A GB2045357B GB 2045357 B GB2045357 B GB 2045357B GB 8006002 A GB8006002 A GB 8006002A GB 8006002 A GB8006002 A GB 8006002A GB 2045357 B GB2045357 B GB 2045357B
Authority
GB
United Kingdom
Prior art keywords
turbine engine
mounting assembly
engine mounting
aircraft turbine
aircraft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB8006002A
Other versions
GB2045357A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Westland Group PLC
Original Assignee
Westland Aircraft Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westland Aircraft Ltd filed Critical Westland Aircraft Ltd
Priority to GB8006002A priority Critical patent/GB2045357B/en
Publication of GB2045357A publication Critical patent/GB2045357A/en
Application granted granted Critical
Publication of GB2045357B publication Critical patent/GB2045357B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pivots And Pivotal Connections (AREA)
GB8006002A 1979-03-06 1980-02-22 Aircraft turbine engine mounting assembly Expired GB2045357B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8006002A GB2045357B (en) 1979-03-06 1980-02-22 Aircraft turbine engine mounting assembly

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7907856 1979-03-06
GB8006002A GB2045357B (en) 1979-03-06 1980-02-22 Aircraft turbine engine mounting assembly

Publications (2)

Publication Number Publication Date
GB2045357A GB2045357A (en) 1980-10-29
GB2045357B true GB2045357B (en) 1982-11-10

Family

ID=26270805

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8006002A Expired GB2045357B (en) 1979-03-06 1980-02-22 Aircraft turbine engine mounting assembly

Country Status (1)

Country Link
GB (1) GB2045357B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2599708A1 (en) * 1986-06-10 1987-12-11 Snecma DEVICE FOR REARLY SECURING A TURBOJET ENGINE ON AN AIRCRAFT MAT
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
EP0431800B1 (en) * 1989-12-05 1994-08-31 ROLLS-ROYCE plc Failure tolerant engine mounting
US5176339A (en) * 1991-09-30 1993-01-05 Lord Corporation Resilient pivot type aircraft mounting
GB2434836B (en) * 2006-02-04 2008-12-10 Rolls Royce Plc Mounting system for use in mounting a gas turbine engine
GB2488555C (en) * 2011-03-01 2014-12-03 A workpiece support comprising pivotal arms

Also Published As

Publication number Publication date
GB2045357A (en) 1980-10-29

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee